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PRODUCTCATALOG
ROKE
TSAN
PRO
DUCT
CAT
ALOG
ENG
2019 ENG-v2
Kemalpaşa Mahallesi Şehit Yüzbaşı Adem Kutlu Sokak No:21 06780 Elmadağ, ANKARA / TURKEYPhone : + 90 (312) 860 55 00Fax : + 90 (312) 863 42 08e-mail : [email protected] : www.roketsan.com.tr
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
www.roketsan.com.tr
PRODUCT CATALOG
INDEXCİRİT 2.75” LASER GUIDED MISSILE 4
YATAĞAN® LASER GUIDED MINIATURE MISSILE SYSTEM 8
CİDA MISSILE 10
KARAOK MAN PORTABLE SHORT RANGE FİRE-AND-FORGET ANTİ-TANK GUIDED MISSILE 12
UMTAS LONG RANGE ANTI-TANK MISSILE SYSTEM 14
L-UMTAS LASER GUIDED LONG RANGE ANTI-TANK MISSILE SYSTEM 18
OMTAS MEDIUM RANGE ANTI-TANK WEAPON SYSTEM 22
TANOK 120 MM LASER GUIDED MISSILE 26
MAM-L SMART MICRO MUNITION 28
MAM-C SMART MICRO MUNITION 30
TEBER LASER GUIDANCE KIT 32
SOM STAND-OFF MISSILE 34
SOM-J JSF-COMPATIBLE STAND-OFF MISSILE 36
ATMACA ANTI-SHIP MISSILE 38
HİSAR AIR DEFENCE MISSILES 40
ARTILLERY ROCKETS 42
TRG-122 GUIDED ROCKET 44
TRG-230 MISSILE 46
TRGK-300 GUIDANCE KIT 48
TRG-300 TIGER MISSILE 50
T-107/122 MULTI-PURPOSE and MULTI BARREL ROCKET LAUNCHER (MBRL) SYSTEM 52
T-122 MULTI BARREL ROCKET LAUNCHER (MBRL) SYSTEM 56
MCL (MULTI-CALIBER LAUNCHER) WEAPON SYSTEM 58
KHAN MISSILE 62
ALKA DIRECTED ENERGY WEAPON SYSTEM 64
ASW ANTI-SUBMARINE WARFARE ROCKETAND LAUNCHER SYSTEM 68
BALLISTIC PROTECTION SYSTEMS 70
BASE BLEED UNIT 76
NAVIGATION SYSTEMS 78
PYROTECHNIC SYSTEMS 96
FUZE SYSTEMS 102
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
CİRİT 2.75”LASERGUIDED MISSILE
5
CİRİT 2.75” LASER GUIDED MISSILE
The 2.75” Laser Guided Missile CİRİT is a highly accurate and cost-effective solution for armed helicopters, optimized for use against stationary or moving lightly armored/unarmored targets. CİRİT has been designed to fill the tactical gap between 2.75” unguided rockets and anti-tank missiles.
CİRİT is stored in a canister to ease loading to the launcher and is fired from a “Smart Launcher”. The launcher is compatible with MIL-STD-8591, MIL-STD-1553 and MIL-STD-1760 interfaces.
CİRİT 2.75” LASER GUIDED MISSILE
*Multi-Purpose Warhead: Anti Armor, Anti-Personnel and Incendiary
* IMU: Inertial Measurement Unit
* MEMS: Micro Electro Mechanical Systems
* SAL: Semi-Active Laser Seeker
Technical Specifications
Diameter 2.75” (70 mm)
Length 1.9 m
Weight 15 kg (without Canister)
Range 1.5 - 8 km
Warhead Types Multi-Purpose Warhead*
High Explosive Warhead
Seeker Mid-course Guidance with MEMS-IMU*
Terminal Guidance with SAL*
Propulsion Min. Smoke Composite Solid Propellant
Target Types Light Armored/Unarmored Vehicles, Infantry Laser Designation
Laser Designators Compatible with STANAG 3733
6
Platforms
CİRİT’s versatile design permits easy integration with different platforms. It has already proven its capabilities in both air-to-surface and surface-to-surface engagement scenarios.
Its Smart Launcher allows for platform and target information to be transferred automatically to the missile prior to firing to enhance the performance envelope. Communication through the Smart Launcher MIL-STD-1760 Interface enables transfer of alignment, utilizing the position and status of the platform, environmental conditions, target coordinates and position of the target.
CİRİT can be integrated into various platforms such as helicopters, UAVs, land vehicles, fixed/towed land platforms, close air-support aircrafts, naval platforms, including coastguard vessels and fast patrol boats. Target designation can be carried out from the firing platform or from any other designator.
7
T-129 ATAK Attack H/C
AH-1W Cobra Attack H/C
Light Attack H/C
UH-60 Utility & Combat H/C
AT-802 Border Patrol Aircraft
HÜRKUŞ-C Light Attack A/C
ANKA-S
BAYRAKTAR TB2
Aerial Platforms
Corvettes
Fast Patrol Boats
Naval PlatformsWheeled/Tracked Armored Vehicle
Stationary Ground Based Launcher
Mobile/Towed Ground Based Launcher
Land Platforms
CİRİT 2.75” LASER GUIDED MISSILE
8
YATAĞAN®
LASER GUIDEDMINIATURE MISSILE
SYSTEM
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
9
YATAĞAN® Laser Guided Miniature Missile System can be fired using new generation man portable 40 mm grenade launcher and has a greater effective range than the maximum range of existing grenade launcher ammunition. Lightweight and small size missile enables integration of the system with mini unmanned aerial vehicles, ground and surface vehicles.
It brings precision, range and target oriented fire power to urban warfare.
YATAĞAN®
LASER GUIDEDMINIATURE MISSILESYSTEM
YATAĞAN® LASER GUIDEDMINIATURE MISSILE SYSTEM
Technical Specifications
Diameter 40 mm
Length ~40 cm
Weight ~1 kg
Maximum Range ~1,000 m
Seeker SAL*
Accuracy (CEP) 1 m
Platforms Grenade Launchers
Mini Unmanned Aerial Vehicles
Unmanned Ground Vehicles
Unmanned Surface Vehicles
*SAL: Semi-Active Laser Seeker
9
10
CİDA MISSILE
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
11
CİDA MISSILE
CİDA Weapon System, which can be classified as a weapon that stands between the advanced guided missiles and unguided rockets, has been designed taking into account the topographic uncertainties of the combat area and the rapid movement of threats during urban operations. It is a lightweight and cost-effective missile that can be guided to its target accurately while ensuring less collateral damage.
CİDA MISSILE
Technical Specifications
Diameter 90 mm
Length 1 m
Weight 7.5 kg
Range 50 - 750 m
Seeker Command to Line-of-Sight (CLOS)
SAL*
Warhead Types Thermobaric
Multi-Purpose Warhead*
High-Explosive Blast Fragmentation
*SAL: Semi-Active Laser
*Multi-Purpose Warhead: Blast Fragmentation, Incendiary and Armor Piercing
12ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
KARAOK MAN PORTABLE SHORT RANGE FİRE-AND
FORGET ANTİ-TANK GUIDED MISSILE
1313
Man Portable Short Range Fire-and-Forget Anti-Tank Guided Missile KARAOK is a portable system that is effective day or night with its Imaging Infrared Seeker.
KARAOK can effectively be used to stop, delay, canalize and neutralize enemy armored and mechanized units at short range during air assault, airborne and amphibious operations.
KARAOKMAN PORTABLE SHORT RANGE FİRE-AND-FORGET ANTİ-TANK GUIDED MISSILE
Missile Technical Specifications
Diameter 125 mm
Weight <16 kg (Missile + Launching Tube)
Range 1,000+ m
Warhead Type Armor Piercing Tandem
Attack Mode Direct/Top Attacks
Operating Mode Fire-and-Forget
KARAOK MAN PORTABLE SHORT RANGE FİRE-AND-FORGET ANTİ-TANK GUIDED MISSILE
14
UMTAS LONG RANGE ANTI-TANK MISSILE SYSTEM
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
15
Long range UMTAS is a anti-tank precision-guided missile system that has been developed for use primarily on attack helicopters.
The missile’s Imaging Infrared Seeker permits its use at day or night, and in adverse weather conditions, and its RF data link provides it with flexible operational capabilities. The missile can be used in fire-and-forget or fire-and-update mode with lock-on before launch or lock-on after launch capabilities. The hitting point on the target can also be updated during flight.
Its precision guidance and control capability, together with its tandem anti-armor warhead, make UMTAS an effective weapon system against armored targets.
UMTAS LONG RANGEANTI-TANK MISSILESYSTEM
UMTAS LONG RANGE ANTI-TANK MISSILE SYSTEM
Technical Specifications
Diameter 160 mm
Length 1.8 m
Weight 37.5 kg
Range 500 – 8,000 m
Seeker IIR*
Warhead Types Tandem Against Reactive Armor
High Explosive Blast Fragmentation
Attack Modes Direct/Top Attacks
Operating Modes Fire-and-Forget Fire-and-Update
Launcher
Missile Capacity 4
Weight 60 kg
Standard Interface MIL-STD-1760
*IIR: Imaging Infrared Seeker
16
System Specifications• Day-Night and All-Weather Operational
Capability
• Effective Against Stationary and Moving Targets
• Capability of Target Update Enables:
- Update of Aim Point on the Target
- Switching Targets During Flight
- Fire Behind Mask
• Insensitive Munition Characteristics Against Fuel Fire and Bullet Impact
17
Platforms
• T129 ATAK Attack H/C
• S70-B SEAHAWK H/C
• HÜRKUŞ-C Light Attack A/C
• Platforms that have MIL-STD-1760 and MIL-STD-1553 Interfaces
UMTAS can be integrated onto naval platforms with stabilized weapon systems, as well as armored vehicles and fixed/towed land platforms.
UMTAS LONG RANGE ANTI-TANK MISSILE SYSTEM
18
L-UMTAS LASER GUIDED LONG RANGE ANTI-TANK
MISSILE SYSTEM
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
19
L-UMTAS LASER GUIDED LONG RANGE ANTI-TANK MISSILE SYSTEM
Technical Specifications
Diameter 160 mm
Length 1.8 m
Weight 37.5 kg
Range 500 – 8,000 m
Seeker SAL*
Warhead Types Tandem Effective Against Reactive Armor
High Explosive Blast FragmentationLauncher
Missile Capacity 4
Weight 60 kg
Standard Interface MIL-STD-1760
L-UMTAS is a long range laser guided anti-tank precision missile system developed primarily for attack helicopter platforms. The laser guidance and tandem armor-piercing warhead features of L-UMTAS ensure its effectivity against both stationary and moving targets. The missile can lock onto the target before launch.
L-UMTAS LASER GUIDED LONG RANGE ANTI-TANK MISSILE SYSTEM
*SAL: Semi-Active Laser
20
System Specifications
• Day-Night Operational Capability
• Lock-On Before Launch (LOBL) or Lock-On After Launch (LOAL)
• Fire Behind Mask
• Effective Against Stationary and Moving Targets
• Insensitive Munition Characteristics Against Fuel Fire and Bullet Impact
21
Platforms
• T129 ATAK Attack H/C
• S70-B SEAHAWK H/C
• HÜRKUŞ-C Light Attack A/C
• Platforms That Have MIL-STD-1760 and MIL-STD-1553 Interfaces
L-UMTAS LASER GUIDED LONG RANGE ANTI-TANK MISSILE SYSTEM
22
OMTAS MEDIUM RANGE ANTI-TANK WEAPON
SYSTEM
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
23
OMTAS is a medium range anti-tank weapon system, effective against armored threats on the battlefield. Its Imaging Infrared Seeker permits its use at day and night, and in adverse weather conditions. The OMTAS Weapon System is composed of a missile, launching platform and a fire control unit, carrying cases and training simulator.
The RF data link between the launcher and missile provides operational flexibility to the user. The missile can be used in fire-and-forget or fire-and-update mode. The hitting point on the target can also be updated during flight.
With precision guidance and its armor piercing tandem warhead, OMTAS ensures effectivity against armored threats.
OMTAS MEDIUM RANGE ANTI-TANK WEAPON SYSTEM
OMTAS MEDIUM RANGE ANTI-TANK WEAPON SYSTEM
* IIR: Imaging Infrared Seeker
Technical Specifications
Diameter 160 mm
Length 1.8 m
Weight 35 kg (Missile + Launch Tube)
36 kg (Tripod Platform)
Range 200 – 4,000 m
Seeker IIR*, Uncooled Type
Warhead Type Tandem Against Reactive Armor
High Explosive Blast Fragmentation
Attack Modes Direct /Top Attacks
Operating Modes Fire-and-Forget
Fire-and-Update
Sight Unit TV/Thermal Camera
24
System Specifications• Day-Night and All-Weather Operational
Capabilities
• Effective Against Stationary and Moving Targets
• Capability of Target Update Enables:
- Update of Aim Point on the Target
- Switching Targets During Flight
- Fire Behind Mask
• Insensitive Munition Characteristics Against Fuel Fire and Bullet Impact
• Fire to the Target Coordinate
• Classroom and Embedded Simulators
• Modular Launching System
• TV/Thermal Camera Unit That Can Be Used Separately
25
Platforms
OMTAS can be used from its own tripod or integrated onto land platforms with open or closed turrets.
OMTAS MEDIUM RANGE ANTI-TANK WEAPON SYSTEM
26
TANOK 120 MM LASER GUIDED MISSILE
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
27
TANOK 120 mm Laser Guided Missile has been developed as an innovative alternative to conventional munitions used in tanks and other artillery guns to have accurate, cost-effective fire power.
TANOK Missile is fulfilling the Armed Forces’ needs to have laser guided anti-tank artillery ammunition. The missile can be fired from land and portable platforms with low weight and soft launch motor.
TANOK 120 MM LASERGUIDED MISSILE
System Specifications• Use in Existing Tanks without any
Modification
• High Hit Probability Against Stationary and Moving Targets with Its Semi-Active Laser Guidance
• Direct/Top Attack Modes
• Effectiveness Against Heavy Armored Threats and Bunkers with Its Tandem Warhead
TANOK 120 MM LASER GUIDED MISSILE
Technical Specifications
Diameter 120 mm
Length 984 mm
Weight 11 kg
Range 1 - 6 km
Seeker SAL*
Warhead Type Armor Piercing Tandem
Targets Heavy and Lightly Armored Vehicles
Platforms Tank, Land Vehicles
*SAL: Semi-Active Laser
28
MAM-LSMART MICRO MUNITION
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
Smart Micro Munition MAM-L has been developed for unmanned aerial vehicles (UAV), light attack aircrafts and air-ground missions for low payload capacity air platforms. MAM-L can engage both stationary and moving targets with high precision.
MAM-LSMART MICRO MUNITION
29
*INS: Inertial Navigation System *GPS: Global Positioning System *SAL: Semi-Active Laser
Technical Specifications
Diameter 160 mm
Length 1 m
Weight 22 kg
Range 8 km (14 km with INS/GPS* Option)
Seeker SAL*
Warhead Types Tandem Effective Against Reactive Armor
High-Explosive Blast Fragmentation
Thermobaric
Fuze Impact
Proximity
Platforms UAVs
Light Attack A/C
MAM-L SMART MICRO MUNITION
30
MAM-CSMART MICRO MUNITION
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
Smart Micro Munition MAM-C has been developed for unmanned aerial vehicles (UAV), light attack aircrafts and air-ground missions for low payload capacity air platforms. MAM-C can engage both stationary and moving targets with high precision.
MAM-CSMART MICRO MUNITION
31
MAM-C SMART MICRO MUNITION
Technical Specifications
Diameter 2.75” (70 mm)
Length 970 mm
Weight 6.5 kg
Range 8 km
Seeker SAL*
Warhead Types Multi-Purpose Warhead*
High-Explosive Blast Fragmentation
Platforms UAVs
Light Attack A/C
*Multi-Purpose Warhead: Blast Fragmentation, Incendiary and Armor Piercing *SAL: Semi-Active Laser
32
TEBERLASER GUIDANCE KIT
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
TEBER is a laser guidance kit for use on MK-81 and MK-82 general purpose bombs. TEBER converts these bombs into precision smart weapons using Inertial Navigation System (INS), Global Positioning System (GPS) and Semi-Active Laser (SAL) Seeker.
An add-on SAL Seeker, mounted on the front section, provides a precise hit capability against moving targets. The Laser Seeker may be equipped with a proximity sensor.
The TEBER tail section is composed of GPS and INS for precise guidance and can be integrated onto the bomb by user in the field. The tail section can also automatically identify the types of the bombs (MK-81/MK-82).
TEBERLASER GUIDANCE KIT
33
TEBER LASER GUIDANCE KIT
Technical Specifications
Length 2.1 m (TEBER-81) 2.6 m (TEBER-82)
Weight ~155 kg (TEBER-81) ~270 kg (TEBER-82)
Range 2 - 28 km
Guidance Modes INS* only INS + GPS* INS + GPS + SAL* INS + SAL*
Warhead Types MK-81 MK-82
Seeker SAL
Proximity Sensor 2-15 m
Accuracy (CEP) <3 m
Maneuverability ± 3 g
Moving Target <50 km/sec Engagement
*INS: Inertial Navigation System *GPS: Global Positioning System *SAL: Semi-Active Laser
34
SOMSTAND-OFF MISSILE
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
35
Stand-Off Missile SOM is an air-to-surface cruise missile fired from beyond the reach of the hostile air defence systems, against heavily defended land or moving naval targets, deep in the battlefield.
SOM (SOM-A / SOM-B1 / SOM-B2)
STAND-OFF MISSILE
*INS: Inertial Navigation System
*GPS: Global Positioning System
*TRN: Terrain Relative Navigation
*IBN: Image-Based Navigation
*ATA: Automatic Target Acquisition
*IIR: Imaging Infrared Seeker
SOM STAND-OFF MISSILE
System Specifications• Low Radar Signature
• Survivable
• Turbojet Engine
• Resistance to Countermeasures/Clutter
• Target of Opportunity Capability
• Selectable Impact Parameters
Length
Weight
Guidance
Range
Warhead Types
Warhead Weight
Seeker
Platforms
~4 m
~600 kg
INS/GPS/TRN*
250+ km
High Explosive Blast/Fragmentation
~230 kg
-
F-4
F-16
~4 m
~600 kg
INS/GPS/TRN/IBN/ATA*
250+ km
High Explosive Blast/Fragmentation
~230 kg
IIR*
F-4
F-16
~4 m
~650 kg
INS/GPS/TRN/IBN/ATA*
250+ km
Tandem Penetrator
~230 kg
IIR*
F-4
F-16
SOM-A SOM-B1 SOM-B2
Technical Specifications
36
SOM-J JSF-COMPATIBLE STAND-OFF MISSILE
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
37
SOM-J is an air-to-surface missile designed to use against heavily defended, high-value maritime and land targets. The missile’s modular design supports necessary operational flexibility.
SOM-J provides enhanced capabilities by building on existing SOM air-to-surface cruise missile technologies already in service with the Turkish Air Force.
SOM-J complements other long range weapon systems and provides an affordable solution to maximize stealth and stand-off across the battlespace.
SOM-J JSF-COMPATIBLE STAND-OFF MISSILE
System Specifications• Low Radar Cross Section
• Survivable
• High Precision Terminal Guidance with IIR Seeker and Data Link
• Resistance to Countermeasures/Clutter
• Network Enabled Weapon (NEW) Capability
• Target of Opportunity Capability
• Selectable Impact Parameters
• In-Flight Retargeting
• Universal Armament Interface (UAI) Compatibility
*INS: Inertial Navigation System
*GPS: Global Positioning System
*TRN: Terrain Relative Navigation
*IBN: Image Based Navigation
*ATA: Automatic Target Acquisition
*IIR: Imaging Infrared Seeker
SOM-J JSF-COMPATIBLE STAND-OFF MISSILE
Technical Specifications
Length ~3,9 m
Weight ~540 kg
Range 150+ nm
Guidance INS/GPS/TRN/ IBN/ATA*
Warhead Type Fragmentation Armor Piercing
Warhead Weight ~140 kg
Seeker IIR*
Platforms F-35 (JSF) F-16
Speed High Subsonic
38
ATMACAANTI-SHIP MISSILE
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
39
ATMACA is a high precision, long range, surface-to-surface, precision strike anti-ship missile which can be integrated to patrol boats, frigates and corvettes.
ATMACA ANTI-SHIP MISSILE
System Specifications• Autonomous
• Low Radar Signature
• High Precision
• All Weather Operational Capability
• Resistant to Countermeasures
• Target Update, Re-Attack, Re-Target and Mission Abort Capability via Data Link
• 3D Mission Planning
• Super Sea Skimming
• Anti-Surface Warfare (ASuW)
*INS: Inertial Navigation System
*GPS: Global Positioning System
ATMACA ANTI-SHIP MISSILE
Technical Specifications
Length 4,800 - 5,200 mm
Weight < 800 kg
Range >200 km
Guidance INS + GPS* + Barometric Altimeter + Radar Altimeter
Warhead Type High Explosive with Penetration
Warhead Weight 250 kg
Seeker Active RF
40
HİSARAIR DEFENCE
MISSILES
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
The HİSAR Air Defense Missiles are operationally used for the protection of military bases, ports, facilities and troops against rotary and fixed wing aircrafts, cruise missiles, air-to-ground missiles and unmanned aerial vehicles (UAV). HİSAR-A and HİSAR-O have a modular structure as part of their family concept, and are designed to be compatible with different platforms, fire control and command control infrastructures.
HİSAR AIR DEFENCE MISSILES
Intercept Range 15 km 25 km
Warhead Types
Seeker
Engine
Types of Targets
High Explosive Fragmentation
Dual Pulse Solid Propellant
Midcourse Guidance with INS* and Data LinkTerminal Guidance with IIR*
Fixed-Wing AircraftsRotary-Wing Aircrafts
Cruise MissilesUAV
Air-to-Ground Missiles
HİSAR-A (Low Altitude)
HİSAR-O(Medium Altitude)
41
Technical Specifications
HİSAR AIR DEFENCE MISSILES
*INS: Inertial Navigation System
*IIR: Imaging Infrared Seeker
System Specifications• Vertical Launch Capability with 360°
Effectiveness
• Dual-Stage Rocket Motor
• Multiplatform Integration Interface
• Thrust Vector Control System
• Impact and Proximity Fuze
• Common Canister and Umbilical Connection Interface for HİSAR-A and HİSAR-O
42
ARTILLERYROCKETS
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
43
ROKETSAN Artillery Rockets provide mass firepower to maneuvering forces with minimum dispersion and maximum warhead effectiveness on targets between 3 - 40 km ranges.
ARTILLERY ROCKETS
ARTILLERY ROCKETS
*HE: High Explosive *PD: Point Detonating
Diameter
Weight
Minimum Range
Maximum Range
Propellant Type Warhead Types
Warhead Weight
Warhead Effective Radius
Fuze Type
107 mm20 kg3 km (at Sea Level) 11+ km (at Sea Level)
Reduced Smoke Composite Solid
HE* + Fragmentation
8.4 kg ≥ 14 m PD*
122 mm66 kg16 km (at Sea Level)21 km (at 600 m above Sea Level)10 km (with Drag Ring)36 km (at Sea Level) 40 km (at 600 m above Sea Level)Composite Solid HE* + Fragmentation
18.4 kg ≥ 20 m PD*
122 mm66 kg16 km (at Sea Level)21 km (at 600 m above Sea Level)10 km (with Drag Ring)36 km (at Sea Level) 40 km (at 600 m above Sea Level)Composite Solid HE* + Steel Ball
18 kg ≥ 40 m PD* and Proximity
TR-107 TR-122 TRB-122
Technical Specifications
Sealed Pod
107 mm and 122 mm Rocket Pod is designed for long term storage. Sealed Pod contains 20 x ready to fire rockets/guided rocket.
It provides advantages such as:• Protection Against Adverse Weather and
Environmental Conditions• Extended Shelf Life• Easy Transportation, Fast and Easy Loading
and Unloading• Quick Reaction Time• Maintenance Free• Built-In Test Capability
44
TRG-122GUIDED ROCKET
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
45
TRG-122 Guided Rocket provides accurate and effective fire power on high priority targets within the ranges 16 - 35 km.
Potential Targets• Targets Located with High Accuracy
• Artillery and Air Defence Systems
• Radar Sites
• Assembly Areas
• Logistic Facilities
• C3 Facilities
• Other High Priority Targets
System Specifications• 7/24 All Weather/Terrain Usage Capability
• Ready to Fire
• Highly Accurate
• Low Collateral Damage
• Precision Strike Capability
• Anti-Jamming/Anti-Spoofing Solutions
TRG-122 GUIDED ROCKET
*GPS: Global Positioning System
*GLONASS: Global Navigation Satellite System
*HE: High Explosive
*PD: Point Detonating
TRG-122 GUIDED ROCKET
Technical Specifications
Diameter 122 mm
Weight 76 kg
Range 16 - 35 km
Guidance GPS* + GLONASS*
Control Aerodynamic Control with Electromechanical Actuation System
Propellant Type Composite Solid
Warhead Types HE* + Steel Ball
Warhead Weight 13 kg
Warhead Effective Radius ≥ 40 m (Steel Ball)
Fuze Type PD* and Proximity
Accuracy (CEP) ≤ 15 m
46
TRG-230MISSILE
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
47
TRG-230 Missile provides accurate and effective fire power on high priority targets within the ranges 20 - 70 km.
TRG-230 Missile can be launched from ROKETSAN TIGER Multi Barrel Rocket Launcher (MBRL) Weapon System, MCL (Multi-Caliber Launcher) Artillery Weapon System and other platforms with compatible interfaces.
System Specifications• 7/24 All Weather/Terrain Usage Capability
• Ready to Fire
• Highly Accurate
• Low Collateral Damage
• Precision Strike Capability
• Anti-Jamming/Anti-Spoofing Solutions
TRG-230 MISSILEPotential Targets• Targets Located with High Accuracy
• Artillery and Air Defence Systems
• Radar Sites
• Assembly Areas
• Logistic Facilities
• C3 Facilities
• Other High Priority Targets
*GPS: Global Positioning System
*GLONASS: Global Navigation Satellite System
*INS: Inertial Navigation System
*HE: High PD and Proximity
*PD: Point Detonating
TRG-230 MISSILE
Technical Specifications
Diameter 230 mm
Weight 210 kg
Range 20 - 70 km
Guidance GPS* + GLONASS* Aided INS*
Control Aerodynamic Control with Electromechanical Actuation System
Propellant Type Composite Solid
Warhead Types HE* + Steel Ball
Warhead Weight 50 kg
Warhead Effective Radius ≥ 55 m
Fuze Type PD* and Proximity
Accuracy (CEP) ≤ 10 m
48
TRGK-300GUIDANCE KIT
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
49
With the installation of the TRGK-300 Guidance Kit on unguided 300 mm rockets, targets within a range of 40 - 90 km can be surpassed with high accuracy.
The guidance kit integration provides a cost-effective solution by using the existing rocket components.
TRGK-300GUIDANCE KIT
*GPS: Global Positioning System
*GLONASS: Global Navigation Satellite System
*HE: High Explosive
*PD: Point Detonating
Technical Specifications of Rocket
Diameter 300 mm
Weight 600 kg
Range 40 - 90 km
Guidance GPS* + GLONASS*
Control Aerodynamic Control with Electromechanical Actuation System
Propellant Type Composite Solid
Warhead Types HE* + Steel Ball
Warhead Weight 150 kg
Warhead Effective Radius ≥ 70 m
Fuze Type PD* and Proximity
Accuracy (CEP) ≤ 50 m
TRGK-300 GUIDANCE KIT
System Specifications• 7/24 All Weather/Terrain Usage Capability
• Ready to Fire
• Highly Accurate
• Increased Effectiveness Against Critical Targets
50
TRG-300TIGER MISSILE
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
System Specifications• Combat Proven
• 7/24 All Weather/Terrain Usage Capability
• Ready to Fire
• Low Collateral Damage
• Long Range Highly Accurate Precision Strike Capability
• Anti Jamming/Anti Spoofing Solutions
TRG-300 TIGER Missile provides accurate and effective fire power on high priority targets within the ranges 20 - 120 km.
TIGER Missile can be launched from ROKETSAN TIGER Multi Barrel Rocket Launcher (MBRL) Weapon System, MCL (Multi-Caliber Launcher) Weapon System and other platforms with compatible interfaces.
Potential Targets• Targets Located with High Accuracy
• Artillery and Air Defence Systems
• Radar Sites
• Assembly Areas
• Logistic Facilities
• C3 Facilities
• Other High Priority Targets
TRG-300TIGER MISSILE
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*BLOCK-II: Enhanced Warhead Dynamic Effectiveness
*GPS: Global Positioning System
*GLONASS: Global Navigation Satellite System
*INS: Inertial Navigation System
*HE: High Explosive
TRG-300 TIGER MISSILE
Technical Specifications BLOCK-I BLOCK-II*
Diameter 300 mm
Weight 585 kg 670 kg
Range 30 - 120 km 20 - 90 km
Guidance GPS* + GLONASS* Aided INS*
ControlAerodynamic Control
with Electromechanical Actuation System
Propellant Type Composite Solid
Warhead Types HE* + Steel Ball
Warhead Weight 105 kg 190 kg
Warhead Effective Radius ≥ 70 m ≥ 80 m
Fuze Type Point Detonating and Proximity
Accuracy (CEP) ≤ 10 m
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T-107/122MULTI-PURPOSE and
MULTI BARREL ROCKET LAUNCHER (MBRL) SYSTEM
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
53
The T-107/122, 107 and 122 mm Multi-Purpose and Multi Barrel Rocket Launcher (MBRL) is a weapon system that provides concentrated and effective fire support against high priority targets in all weather and terrain conditions during day and night.
Highly maneuverable T-107/122 MBRL can fire TR-107, TR-122, TRB-122 Rockets and TRG-122 Missiles.
The T-107/122 MBRL Battery consists of Command & Control Vehicle, Ammo Supply Vehicle, Meteorology Vehicle, Maintenance & Repair Vehicle and other auxiliary vehicles.
T-107/122MULTI-PURPOSE and MULTI BARREL ROCKET LAUNCHER (MBRL) SYSTEM
Technical Specifications
Diameter 107 mm and 122 mm
Range 3 - 40 km
Number of Tubes 3x20 TR-107 1x20 TR-122, TRB-122, TRG-122
Salvo Interval 0.5 ~ 2 sec
Vehicle 4x4 or 6x6 Tactical Wheeled Vehicle
Aiming Automatic Manual (Back-Up)
Stabilization 4 Hydraulic Legs
Vehicle Navigation INS*/GPS* System
*INS: Inertial Navigation System
*GPS: Global Positioning System
T-107/122 MULTI-PURPOSE and MULTI BARREL ROCKET LAUNCHER (MBRL) SYSTEM
System Specifications• Onboard Crane for Ammunition Supply
• Automatic Aiming
• Communication System (Wired/Wireless – Voice/Data)
• Hydraulic Stabilization System
• Integrated Ground Meteorology System
• Cabin Pressurization System (Optional)
• Power Supply and Distribution System
• Inside Cabin or Remote Firing Capability
• Ready to Fire in Maximum 5 Minutes
• Ballistic Protection (Optional)
• Capability of Firing at Negative Elevation
5454
T-107/122 MBRL Battery Structure
The T-107/122 MBRL Battery is capable of performing independent missions with its mission support vehicles.
T-107/122 Battery is composed of 1 x C-107/122 Command & Control Vehicle, 6 x T-107/122 Launchers, 6 x L-107/122 Ammo Supply Vehicles, 1 x M-107/122 Meteorology Vehicle and 1 x R-107/122 Repair Vehicle. The number and type of vehicles can be customized according to the customer's requirements.
T-107/122 MBRL Battery Organization
The Command & Control System and Weapon Management System of the battery can be integrated with modern fire support automation (tactical fire direction system) and battlefield command-control and management systems. Target acquisition radars or Unmanned Aerial Vehicles supply target information to the Battery.
Integration with Tactical Fire Direction System,
Battlefield C2 and Management System and Target Acquisition Systems
R-107/122 Repair Vehicle
6 x L-107/122Ammo Supply
Vehicles
6 x T-107/122Launchers
M-107/122 Meteorology Vehicle
C-107/122 Command & Control Vehicle
Fire Support Command Control System
Target Acquisition
RadarQuick Fire
Channel
Technical Fire Direction
System Technical Fire Direction
System
Quick Fire Channel
Tactical Fire Direction System
LauncherFire Control System
Battery C2 Vehicle Command Control System
Forward Observer
NATO & C4I Systems
UAV
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Shoot and Scoot Capability
The T-107/122 Launcher perfectly performs “shoot and scoot tactics” with its inertial and global navigation and automatic aiming systems.
• Capability to fire within 5 minutes after deploying
• Capability to displace in 5 minutes after firing
• Capability to carry out multiple firing missions in a short period of time.
Negative Elevation
The T-107/122 is able to fire the 107 mm rockets at negative elevations in mountainous areas to targets below the launcher's altitude.
Direct Fire Capability (Optional)• TR-107 Rockets can be fired directly by
using direct fire control unit inside the cabin.
• Launcher’s hydraulic support legs, help the dispersion to be kept at a minimum level.
• With its massive fire capability, the T-107/122 Launcher can be used not only to suppress target areas, but it can also be used against point targets effectively.
High Mobility Capability
The T-107/122 Launcher Platform is a 4x4 or 6x6 tactical wheeled vehicle, which provides superior on-road and off-road capability. Its compact and robust structure provides a reliable launching platform.
Minimum Crew
Due to the fully automatic navigation and aiming systems, the T-107/122 can be operated with two crew, launcher commander and driver.
55
T-107/122 MULTI-PURPOSE and MULTI BARREL ROCKET LAUNCHER (MBRL) SYSTEM
56
T-122 MBRL MULTI BARREL
ROCKET LAUNCHER (MBRL) SYSTEM
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
The T-122, 122 mm Multi Barrel Rocket Launcher (MBRL) is a weapon system that provides concentrated and effective fire support against high priority targets in all weather and terrain conditions during day and night.
The T-122 MBRL System can provide indirect firepower within a range of 16 - 40 km.
T-122 MBRL MULTI BARREL ROCKET LAUNCHER (MBRL) SYSTEM
57
System Specifications• Steel or Composite Pods• Onboard Crane for Ammunition Supply• Automatic Aiming• Communication System
(Wired/Wireless – Voice/Data)• Hydraulic Stabilization System• Integrated Ground Meteorology System• Cabin Pressurization System (Optional)• Power Supply and Distribution System• Firing Inside Cabin or Remote Firing Capability• Ready to Fire within 5 Minutes• Ballistic Protection (Optional)• Combat Proven• 7/24 All Weather/Terrain Usage Capability• Increased Responsiveness • Increased Effectiveness Against Critical
Targets• Air, Rail and Sea Transportable• Three Man-Crew
T-122 MBRL MULTI BARREL ROCKET LAUNCHER (MBRL) SYSTEM
*INS: Inertial Navigation System *GPS: Global Positioning System
Technical Specifications
Diameter 122 mm
Range 16 - 40 km
Number of Tubes 2x20 TR-122, TRB-122, TRG-122
Salvo Interval 0.5 sec
Vehicle 6x6 Tactical Wheeled Vehicle
Elevation 0 - 55°
Deflection ±110°
Aiming Automatic Manual (Back-Up)
Stabilization 4 Hydraulic Legs
Vehicle Navigation INS*/GPS* System
Fire Control System
The Fire Control System of T-122 MBRL System provides mission critical advantages.
• Computer Aided-Deployment
• Fire Planning
• Technical Fire Direction
• Situational Awareness
• Digital Integration to other Fire Support Systems
• Digital Mapping
• Digital Communication
• User friendly interface
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MCL (MULTI-CALIBER LAUNCHER) WEAPON
SYSTEM
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
59
MCL (Multi-Caliber Launcher) Weapon System is capable of providing precise fire on critical targets between 16 - 280 km range.
MCL Weapon System is a highly maneuverable fire support system that can fire TR-122, TRB-122, TRG-122, TRG-230, TRG-300, TRGK-300 and KHAN Rockets and Missiles. The battery is composed of Command & Control Vehicle, Launchers, Ammo Supply Vehicles, Meteorology Vehicle and Maintenance & Repair Vehicle, as well as other mission vehicles needed.
MCL (MULTI-CALIBER LAUNCHER) WEAPON SYSTEM
MCL (MULTI-CALIBER LAUNCHER)WEAPON SYSTEM
*INS: Inertial Navigation System
*GPS: Global Positioning System
System Specifications• Steel or Composite Pods
• Onboard Crane for Ammunition Supply (Optional)
• Automatic Aiming
• Communication System (Wired/Wireless – Voice/Data)
• Hydraulic Stabilization System
• Integrated Ground Meteorology System
• Cabin Pressurization System (Optional)
• Power Supply and Distribution System
• Firing from the Cabin or Remote Firing Capability
• Ready to Fire within 5 Minutes
• Ballistic Protection (Optional)
Technical Specifications
Diameter 122 mm, 230 mm, 300 mm and 610 mm
Range 10 - 280 km
Number of Tubes 2x20 TR-122, TRB-122, TRG-122 2x6 TRG-230 2x4 TRG-300, TRGK-300 1x KHAN
Salvo Interval 0.5 - 15 sec
Vehicle 6x6 or 8x8 Tactical Wheeled Vehicle
Aiming Automatic Manual (Back-Up)
Stabilization 4 Hydraulic Legs
Vehicle Navigation INS*/GPS* System
122 mm (TR/TRB/TRG-122)2 Pods (2 x 20=40 Rockets/ Guided Rockets)
230 mm (TRG-230) 2 Pods (2 x 6=12 Missiles)
610 mm (KHAN)1 Pod (1 Missile)
300 mm (TIGER) 2 Pods (2 x 2=4 Missiles)
6060
Battery Structure
The MCL Weapon System Battery is capable of performing independent missions with its mission support vehicles. A typical MCL Weapon System battery is composed of 1 x Command & Control Vehicle, 6 x Launcher Vehicles, 6 x Ammo Supply Vehicles, 1 x Meteorology Vehicle and 1 x Maintenance & Repair Vehicle. The number and type of vehicles can be customized.
Battery Organization
The Command & Control System and Weapon Management System of the battery can be integrated with modern fire support automation (tactical fire direction system) and battlefield command-control and management systems. Target acquisition radars or Unmanned Aerial Vehicles supply target information to the Battery.
Integration with Tactical Fire Direction System,
Battlefield C2 and Management System and Target Acquisition Systems
Meteorology Vehicle
Command & Control Vehicle
Repair Vehicle6 x Ammo Supply Vehicles
6 x Launchers
Ease of Use
Transportability
Flexibility
DeterrentForce
LogisticSupportability
Survivability
Mobility
Interoperability
Shoot and Scoot
• Ergonomy• User Friendly GUI• Automated System &
Minimum Crew
• Long Range & Mass Fire Capability
• Wide Range and Area Coverage
• Precision Fire
• Situational Awareness• Safe and Secure
Communication• Anti Jamming/Anti
Spoofing Solutions
• Fast Deployment & Redeployment
• Short Preparation Time to Fire
• Integration to NATO & C4I Systems
• All Terrain Conditions
• Multiple Caliber • Autonomous• Day & Night Operational
Capability• All Weather
• Compact Structure• Land, Rail, Sea and Air
Transportation
• High Reliability & Operational Readiness
• Long Shelf Life & Life Extention
• Training and Training Aids • Long Term Logistic Support • Tailored Solutions
6161
Deterrent Force
The system is a deterrent force due to its long range and mass fire capabilities. It can therefore perform vital tasks in a wide range of missions from peace keeping, defence and to attack operations for the support of a maneuvering force.
High Survivability
The system provides high survivability on the battlefield with its quick aiming and displacement capability, shoot and scoot ability, high mobility and secure digital & voice communication system.
Transportability
The system can be transported by land, air, sea and railways.
It is transportable by almost all types of cargo planes.
High Mobility
The Launcher Vehicle is a 6x6 or 8x8 tactical wheeled vehicle, which provides superior on-road and off-road travel capability. Its compact and robust structure provides a reliable launching platform.
Shoot and Scoot Capability
The Launcher perfectly performs “shoot and scoot” with its inertial and global navigation and automatic aiming systems.
• Capability to fire within 5 minutes after deploying
• Capability to displace in 5 minutes after firing
• Capability to carry out multiple firing missions in a short period of time
MCL (MULTI-CALIBER LAUNCHER)WEAPON SYSTEM
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KHAN MISSILE
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
63
KHAN Missile provides accurate and effective fire power on strategic targets within the battlefield.
The missile can be launched from 8x8 Tactical Wheeled Vehicle, ROKETSAN MCL (Multi-Caliber Launcher) Artillery Weapon System and other platforms with compatible interfaces.
Potential Targets• Targets Located with High Accuracy
• Artillery and Air Defence Systems
• Radar Sites
• Assembly Areas
• Logistic Facilities
• C3 Facilities
• High Priority Targets
KHAN MISSILE
Technical Specifications
Diameter 610 mm
Weight 2,500 kg
Range 80 - 280 km
Guidance GPS* + GLONASS* Aided INS* INS* Only
Control Aerodynamic Control with Hydraulic Actuation System
Propellant Type Composite Solid
Warhead Type HE* Blast Fragmentation
Warhead Weight 470 kg
Fuze Type PD* and Proximity
Accuracy (CEP) ≤ 10 m GPS + GLONASS Aided INS* ≤ 100 m INS* Only
KHAN MISSILE
*GPS: Global Positioning System
*GLONASS: Global Navigation Satellite System
*INS: Inertial Navigation System
*HE: High Explosive
*PD: Point Detonating
Sealed Pod
Features• Combat Proven
• 7/24 All Weather/Terrain Usage Capability
• Ready to Fire
• Low Collateral Damage
• Long Range Highly Accurate Precision Strike Capability
• Anti Jamming/Anti Spoofing Solutions
64
ALKADIRECTED ENERGY
WEAPON SYSTEM
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
ALKA DIRECTED ENERGY WEAPON SYSTEM
65
ALKA Directed Energy Weapon System (DEWS) neutralizes or totally destructs targets such as Improvised Explosive Devices (IED), mini/micro unmanned aerial vehicles (UAV), drones, mini/micro unmanned aerial vehicles (UAV) carrying a variety of payloads (camera, explosives, etc.) as well as swarm attacks.
ALKA DIRECTED ENERGYWEAPON SYSTEM
Drone
Swarm Destruction Destruction Interception
IED*Precise
TrackingSwarm
Interception
* EJS: Electromagnetic Jamming System
* EDS: Electromagnetic Destruction System
* IED: Improvised Explosive Device
System Specifications• Automatic Aiming to Target Detected by
Radar
• Automatic Target Detection and Tracking Through Artificial Intelligence Assisted Image Processing (Minimum False Alarm Rate)
• Standalone Use without Radar
• EJS* 4,000 m
• Effective Laser Destruction Range 500 m
• Effective Destruction Range of 1,000 m with EDS*
• Independent of Number of Targets, Interception Capability Against Swarm Attacks
• Selection of Precise Destruction Point on the Target
• Tracking and Destruction of High Speed Targets (150 km/hr)
• High Precision Target Tracking (8 mm Precision at 1,000 m)
• Multiple Target Tracking
• Day/Night Operations
• Surveillance Only Mode
• Reduction of Operator Cognitive Workload through Neuro-Ergonomics Approach
• Low Cost per Shot
• Successive Firing Capability
66
Areas of Use
• Urban Operations (against IEDs)
• Protection of Military Units
• Protection of Government Buildings
• Protection of Airports
• Protection of Residential Areas
• Protection of High-Tech Production Facilities
• Protection of Power Plants
• Protection of VIP
• Protection of Other Critical Facilities
67
Mobile Use
• Ability to Perform on 4X4 Vehicle
• Operation within the Cabin
• Internal Power Unit
• Modular Configuration
• Deployment on Desired Location
• Easy Operation with 2 Personnel
Stationary Use
• Tower or Shelter Configuration
• Remote Operation from the Command Center
• Use of External Power Sources
• Easy Operation with Single Personnel
ALKA DIRECTED ENERGY WEAPON SYSTEM
68
ASWANTI-SUBMARINE
WARFARE ROCKET AND LAUNCHER SYSTEM
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
Anti-Submarine Warfare (ASW) Rocket and Launcher System can be deployed on patrol boats and engage undersea targets at 500 - 2,000 m ranges and in 15 - 300 m depth. Stabilized Launcher has automatic laying (manual as back-up) system which works in couple with vessel’s combat management system and sonar.
The system can fire insensitive munition class rockets in single or in salvo, and its time setting fuze enables the rockets to detonate at the desired depth.
The fire control system utilizes the navigation and target data provided by the vessel and calculates the necessary firing data.
ASWANTI-SUBMARINEWARFARE ROCKET AND LAUNCHER SYSTEM
69
Diameter 196 mm
Weight (Rocket) 35.5 kg
Explosive Weight 12 kg
System Weight 1,200 kg (with Rockets)
Length (Rocket) 1.3 m
Range 500 - 2,000 m
Depth of Detonation 15 - 300 m
Warhead Type HE*
Fuze Type Time Setting (Depth Setting by Fire Control Computer)
Salvo Interval 0.8 sec
Propellant Type Reduced Smoke Composite Propellant
Launcher System Stabilized, Automatic Launcher Laying Using Vessel Sonar Data
Number of Rockets 6 in the Launcher
Launcher Laying Automatic Manual (Back-up)
Technical Specifications
ASW ANTI-SUBMARINE WARFARE ROCKET AND LAUNCHER SYSTEM
*HE: High Explosive
70
BALLISTICPROTECTION SYSTEMS
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
71
BALLISTICPROTECTION SYSTEMSROKETSAN Ballistic Protection Center (BPC) has been established to fulfill the ballistic protection requirements of military and civilian platforms. BPC is capable of designing, developing, producing and testing composite and explosive reactive armors (ERA) for lightly and heavy armored vehicles. It also provides force protection and Elastic Layered Armor System solutions to increase protection level of armored vehicles against RPG threats.
BALLISTIC PROTECTION SYSTEMS
Technical Specifications
• Heavy Armor Ceramic Block Production
• Oxide and Non-Oxide Ceramic Armor Production Infrastructure
• Infrastructure for Production of Passive Armor Materials
• Advanced Ceramics: AI203, Sic, Hp-B4c, etc.
• Support Materials: Aramide, Ultmwpe, S2 Glass, etc.
• High Hardness Ceramic Grinding, Cutting Confinement and Armor Welding Infrastructure
• Insensitive Reactive Armor Explosive Material Production
• Armor Integration Facility
72
ERA
ERA system is a hybrid armor system developed to increase survivability of armored combat vehicles and their modernization.
Different energetic material technologies, from those developed for main battle tanks, to self-limiting reactive armor, to light armored vehicles are employed in ERA.
System Specifications
• Maximum Protection Against Anti-Tank Missiles (ATGM) and RPG Type Threats
• Protection Against Tandem Warheads
• Insensitive Explosive
• Minimum Collateral Damage
• Modular System – Easy Mounting and Dismounting
• Applicable on Different Type Vehicles
• No Maintenance Required
Reactive Armor on Wheeled Armored Vehicle
Reactive Armor on Tracked Armored Vehicle
Reactive Armor on Main Battle Tank
73
Armor Kits Against Mine and Improvised Explosive Devices
Due to Mines and Improvised Explosive Devices (IED) being among the primary threats against military units, ROKETSAN has developed various ballistic protection systems, including armor and protection systems of the ALTAY Main Battle Tank. These systems have been designed in compliance with armored vehicles in the inventory of Turkish Armed Forces and tested in accordance with STANAG 4569 AEP 55 Volume 2 and Volume 3. The mine kits provide protection against mines in accordance with STANAG Levels II-IV.
Composite Armor System
Composite Armor System is a modern and light protection solution for kinetic and shaped charge ammunition and can be installed on land, naval and air platforms. At BPC ROKETSAN produces both passive composite armor plates from ceramic powder, and reactive armor plates from energetic materials with integrated armor modules.
BALLISTIC PROTECTION SYSTEMS
74
Base Protection
Base Protection Systems provide modular, portable and easily mountable ballistic protection against various threats for military camps. They also protect the critical facilities and areas against kinetic energy ammunition, mortar and RPG threats.
Force Protection System (RZB-20/20B)
The patented RZB-20/20B Composite Armor Block developed by ROKETSAN BPC for increasing the protection of bases is especially designed to protect against effects of light weapons, shrapnel and high explosives. Due to its modular structure, it can be easly installed and replaced.
75
Force Protection Systems (RZP-10)
RZP-10, developed for the protection of containers against blast effect and shrapnel of mortar rounds, is a protection panel integrated to reinforced containers with elevated roof. The patented RZP-10 can be easily installed due to its modular structure.
Force Protection Systems (RZK-7)
RZK-7, used with Composite Armor Blocks, has a caged structure and is part of the Force Protection Systems. RZK-7 can easily be positioned and relocated due to its modular structure.
BALLISTIC PROTECTION SYSTEMS
76
BASEBLEED UNIT
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
77
BASEBLEED UNITBase Bleed Unit is used to increase the 155 mm Artillery Shell’s range.
Base Bleed Unit increases the range of the 155 mm MOD274 shell by approximately 30%.
Diameter 155 mm
Range of MOD274 39+ km with Base Bleed Unit
Propellant Type Composite Solid Propellant
Technical Specifications
Approx. 30% More Range
BASE BLEED UNIT
without Base Bleed Unit
with Base Bleed Unit
78ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
ALBATROS MODULAR INTEGRATED
INERTIAL NAVIGATION SYSTEM
ROKETSAN
79
ALBATROS MODULAR INTEGRATEDINERTIAL NAVIGATION SYSTEM
ALBATROSMODULAR INTEGRATEDINERTIAL NAVIGATIONSYSTEMITAR free ALBATROS is a modular integrated Inertial Navigation System (INS), which can utilize different Inertial Measurement Units (IMU) and Global Navigation Satellite System (GNSS) receivers. Modular architecture provides the capability to integrate the existing compatible IMUs and GNSS receivers. In addition, TurNa TM/TQ/N IMUs and ALDEBARAN/ANTARES GNSS receivers can be used in ALBATROS to obtain the INS that meets the system requirements.
ALBATROS can be integrated into different platforms (missiles, guided munitions, unmanned aerial vehicles, air and land platforms, naval vessels, etc.) due to its modular architecture.
Horizontal & Vertical Positioning Accuracy Horizontal Position (CEP) Vertical Position (PE) Inertial + GNSS* ≤ 10 m ≤ 10 mFree Inertial (Land Application) ≤ 0.5 nm/hr ≤ 0.5 nm/hrFree Inertial ≤ 10 nm/hr ≤ 10 nm/hr
Environmental Specifications Compatible with MIL-PRF-71185A (AR), MIL-STD-810G and MIL-STD-461E standards.
Mechanical Specifications DimensionsMass
210 mm x 210 mm x 165 mm< 4.7 kg
Technical Specifications
*GNSS : Global Navigation Satellite System (GPS, GLONASS, GALILEO, BEIDOU etc. globally positioned satellite based navigation systems)
ROKETSAN
ROKETSAN
80ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
ALDEBARANGPS and GLONASS
RECEIVER
ROKETSAN
81
ALDEBARAN GPS and GLONASSRECEIVER
ALDEBARAN GPS and GLONASS RECEIVER
ITAR free ALDEBARAN is a Global Navigation Satellite System (GNSS) receiver which can work with passive or active antennas, designed to perform under high dynamics (velocity, acceleration and altitude). The receiver which utilizes Global Positioning System (GPS) and GLONASS satellite systems, has a software-based structure, thus can be adapted to different platform (missile, guided munitions, unmanned aerial vehicle, land vehicle, etc.) requirements.
Performance Specifications
Channel Configuration GPS L1 C/A, GLONASS L1 C/A, SBAS L1 C/A
Horizontal Position ≤ 10 m (RMS) Accuracy
Vertical Position ≤ 15 m (RMS) Accuracy
Dynamic Range
Velocity ≥ 1,400 m/sec
Altitude ≥ 40,000 m
Mechanical Specifications
Dimensions Ø 149 mm x 49 mm
Mass 826 g
Environmental Specifications
Compatible with MIL-STD-810G and MIL-STD-461E standards.
Technical Specifications
ROKETSAN
ROKETSAN
82ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
ANTARESGPS and GLONASS
RECEIVER
ROKETSAN
83
ANTARES GPS and GLONASSRECEIVERANTARES is a Global Navigation Satellite System (GNSS) receiver designed to perform under high dynamics (velocity, acceleration and altitude). The receiver which utilizes Global Positioning System (GPS) and GLONASS satellite systems, has a software-based structure, thus can be adapted to different platform (missile, guided munitions, unmanned aerial vehicle, land vehicle etc.) requirements. With its innovative architecture, ANTARES can be integrated with new capabilities such as different satellite constellations and internal anti-jamming.
Performance Specifications
Channel Configuration GPS L1 C/A, GLONASS L1 C/A
Position ≤ 10 m (RMS) Accuracy (3D)
Dynamic Range
Velocity ≥ 1,400 m/sec
Altitude ≥ 40,000 m
Mechanical Specifications
Dimensions Ø 108 mm x 38 mm
Mass 340 g
Environmental Specifications
Compatible with MIL-STD-810G and MIL-STD-461E standards.
Technical Specifications
ANTARES GPS and GLONASS RECEIVER
ROKETSAN
ROKETSAN
84ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
RAL2000 NAVIGATION GRADE RLG
BASED INERTIALMEASUREMENT UNIT
85
RAL2000 NAVIGATION GRADE RLG BASED INERTIAL MEASUREMENT UNIT
RAL2000 NAVIGATION GRADE RLG BASED INERTIAL MEASUREMENT UNITThe RAL2000 is a navigation grade Inertial Measurement Unit (IMU) developed for long range missiles in addition to land, sea and air platforms, including unmanned aerial vehicles. The RAL2000 could satisfy high navigation performance and adverse environmental requirements through its optimized system design, Ring Laser Gyroscopes and Quartz Pendulum Accelerometers. It is the upgraded version of RNU-100M in terms of mass and volume.
Technical Specifications1
Sensor Quartz Pendulum Accelerometer Ring Laser Gyroscope3
Performance SpecificationsMeasurement Range ± 22 g ± 400 °/secResidual Bias Error (1σ) < 25 μg < 0.04 °/hr
Mechanical Specifications2 DimensionsMass
IMU: Inertial Measurement Unit
1 IEEE-528-2001
2 IEEE-1293-1998
3 IEEE-647-2006
265 mm x 255 mm x 230 mm< 16 kg
Environmental SpecificationsCompatible with MIL-STD-810G and MIL-STD-461E standards.
86ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
RNL2000-KRLG BASED INERTIAL LAND
NAVIGATION SYSTEM
87
RNL2000-K RLG BASED INERTIAL LAND NAVIGATION SYSTEM
RNL2000-KRLG BASED INERTIAL LANDNAVIGATION SYSTEM
RNL2000-K is a navigation grade Inertial Measurement Unit (IMU) capable of satisfying the high navigation performance and adverse environmental requirements through optimized system design and Ring Laser Gyroscopes.
The ITAR free RNL2000-K can be integrated into air, underwater and surface platforms with auxiliary aiding systems.
Optionally, RNL2000-K can be provided with Navigation Control and Visualization Unit (NCVU).
*GNSS : Global Navigation Satellite System (GPS, GLONASS, GALILEO, BEIDOU etc. globally positioned satellite based navigation systems)
*ZUPT: Zero Velocity Update
*DT: Distance Traveled
Horizontal & Vertical Positioning Accuracy Horizontal Position (CEP) Vertical Position (PE)Inertial + GNSS* ≤ 10 m ≤ 10 mFree Inertial ≤ 18 m ≤ 10 m(ZUPT* period: 4 min.) (DT* ≤ 27 km) (DT ≤ 35 km)
Technical Specifications
Mechanical Specifications DimensionsMass
265 mm x 255 mm x 230 mm< 15.5 kg
88
RNU-100MNAVIGATION GRADE
RLG BASED INERTIAL MEASUREMENT UNIT
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
89
RNU-100MNAVIGATION GRADE RLG BASED INERTIAL MEASUREMENT UNIT
RNU-100M NAVIGATION GRADE RLG BASED INERTIAL MEASUREMENT UNIT
RNU-100M is a navigation grade Inertial Measurement Unit (IMU) developed for land, aerial and naval platforms. RNU-100M could satisfy high navigation performance and adverse environmental requirements through optimized system design, Ring Laser Gyroscopes and Quartz Pendulum Accelerometers.
Sensor Quartz Pendulum Accelerometer2 Ring Laser Gyroscope3
Performance SpecificationsMeasurement Range ± 22 g ± 400 °/secResidual Bias Error (1σ) < 25 μg < 0.04 °/hr
Technical Specifications1
Mechanical SpecificationsDimensionsMass
315 mm x 420 mm x 240 mm22 kg
1 IEEE-528-2001
2 IEEE-1293-1998
3 IEEE-647-200
90ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
TurNa-NNAVIGATION GRADE
FOG BASED INERTIAL MEASUREMENT UNIT
ROKETSAN
91
TurNa-N NAVIGATION GRADE FOG BASED INERTIAL MEASUREMENT UNITTurNa-N is a navigation grade Inertial Measurement Unit (IMU) consisting of 3 Fiber Optic Gyroscopes (FOG) and 3 Quartz Pendulum Accelerometers. TurNa-N is designed for high performance under harsh environmental conditions, thus can be used on different platforms such as land vehicles, fire control systems, unmanned aerial vehicles and naval vessels.
With its high performance, TurNa-N can satisfy both Global Navigation Satellite System (GNSS) aided and pure inertial navigation (0.8 nm/hr) requirements.
Technical Specifications1
TurNa-N NAVIGATION GRADE FOG BASEDINERTIAL MEASUREMENT UNIT
Sensor Quartz Pendulum Accelerometer2 Fiber Optic Gyroscope3
Performance SpecificationsMeasurement Range ± 30 g ± 250 °/secResidual Bias Error (1σ) < 50 µg < 0.04 °/hr
Mechanical SpecificationsDimensionsMass
286 mm x 160 mm x 160 mm< 9.4 kg
Environmental SpecificationsCompatible with MIL-STD-810G and MIL-STD-461E standards.
1 IEEE-528-2001
2 IEEE-1293-1998
3 IEEE-952-1997
ROKETSAN
ROKETSAN
92ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
TurNa-TQTACTICAL GRADE
FOG BASED INERTIAL MEASUREMENT UNIT
ROKETSAN
93
TurNa-TQ TACTICAL GRADE FOG BASED INERTIAL MEASUREMENT UNIT TurNa-TQ, containing 3 Fiber Optic Gyroscopes (FOG) and 3 Quartz Pendulum Accelerometers, is a tactical grade Inertial Measurement Unit (IMU) which can be used in different guidance, control and navigation applications. TurNa-TQ has high performance under harsh environmental conditions and can be used in different platforms. TurNa-TQ can be used in missiles, guided munitions, stabilized platforms, unmanned aerial vehicles and on their flight computer systems.
TurNa-TQ TACTICAL GRADE FOG BASED INERTIAL MEASUREMENT UNIT
Technical Specifications1
Sensor Quartz Pendulum Accelerometer2 Fiber Optic Gyroscope3
Performance SpecificationsMeasurement Range ± 60 g ± 490 °/secResidual Bias Error (1σ) < 1 mg < 1 °/hr
Mechanical Specifications DimensionsMass
Ø 127 mm x 79 mm1.3 kg
Environmental SpecificationsCompatible with MIL-STD-810G and MIL-STD-461F standards.
1 IEEE-528-2001
2 IEEE-1293-1998
3 IEEE-952-1997
ROKETSAN
ROKETSAN
94ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
TurNa-TMTACTICAL GRADE
FOG BASED INERTIAL MEASUREMENT UNIT
ROKETSAN
95
TurNa-TM TACTICAL GRADE FOG BASED INERTIAL MEASUREMENT UNIT
TurNa-TM TACTICAL GRADE FOG BASED INERTIAL MEASUREMENT UNIT TurNa-TM, containing 3 Fiber Optic Gyroscopes (FOG) and 3 Micro Electro Mechanical Systems (MEMS) accelerometers, is a tactical grade Inertial Measurement Unit (IMU) which can be used in different guidance, control and navigation applications. TurNa-TM has high performance under harsh environmental conditions and can be used on different platforms. TurNa-TM can be used in missiles, guided munitions, stabilized platforms, unmanned aerial vehicles and on their flight computer systems.
Sensor MEMS* Accelerometer2 Fiber Optic Gyroscope3
Performance SpecificationsMeasurement Range ± 10 g a ± 30 g b
Residual Bias Error (1σ) < 0.33 mg a < 0.66 mg b
± 490°/sec
< 1 °/hr
Technical Specifications1
Mechanical Specifications DimensionsMass
Ø 127 mm x 79 mm1.2 kg
Environmental SpecificationsCompatible with MIL-STD-810G and MIL-STD-461F standards.
1 IEEE-528-2001
2 IEEE-1431-2004
3 IEEE-952-1997
(a,b): In different axes TurNa-TM performance specifications
* MEMS: Micro Electro Mechanical Systems
ROKETSAN
ROKETSAN
96ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
97
Rocket Motor Igniters & Safe and Arm Devices (SAD)
Rocket Motor Igniters
• Designed for Solid Propellant Rocket Motors (with or without SAD)
• Designed for Turbojet Motors
• Complies with MIL-STD-1901A, MIL-STD-1576, STANAG 4368
• Safe to Electrostatic Discharge (AECTP-500)
• Complies with Electromagnetic Compatibility Standards (MIL-STD-464A/461F)
• 1W/1A/5 Minutes No Fire, High Reliability
Safe and Arm Devices (SAD)
• Arm - Safe Signal
• Arm - Safe Indicator
• Manual / Remote Control
• Arming Time for EM-SADs <250 ms
• -40 to +70°C Operation Temperature
• Adjustable Interfaces (Mechanical or Electrical)
PYROTECHNIC SYSTEMS
EM-EKM100 EM-EKM200 EM-EKM300 E-EKM400 EM-EKM500 EM-EKM600
PYROTECHNIC SYSTEMS
98
Initiators & Power CartridgesHighly reliable, low cost and light weight low voltage hot-bridgewire initiators are used for initiations of rocket motor igniters, gas generators, and pyrotechnic devices.
Squibs RSKM-100 RSKU-100 RSKT-200 RSKKOM-100 RSKKOM-110
Bridgewire Resistance 1.1 ± 0.1 Ω 0.6 ± 0.1 Ω 2.15 ± 0.15 Ω 1.15 ± 0.1 Ω 1.15 ± 0.1 Ω
Max. No-Fire (5 min.) 1 A/1 W 1 A/1 W 0.35 A 1 A/1 W 1 A/1 W
All Firing Current 3.5 A (50 ms) 3.5 A (50 ms) 1.2 A (10 ms) 3.5 A (50 ms) 3.5 A (50 ms)
Function Time < 5 ms < 25 ms < 10 ms < 5 ms < 5 ms
Output (16,4 cc chamber) 1.5 MPa 1.5 MPa 1.5 MPa 0.7 MPa 0.7 MPa
Electrical Interface Pin Type Pin Type Pin Type Pin Type Pin Type
Operational Temperature -60 / +70ºC -60 / +70ºC -35 / +60ºC -60 / +70ºC -60 / +70ºC
Environmental Tests MIL-DTL-23659 MIL-DTL-23659 MIL-DTL-23659 MIL-DTL-23659 MIL-DTL-23659
Power Cartridges RS-GK100 RS-GK200 RS-GK400
Bridgewire Resistance 1.15 ± 0.2 Ω (Dual BW) 1.15 ± 0.2 Ω (Dual BW) 1.15 ± 0.2 Ω (Dual BW)
Max. No-Fire (5 min.) 1 A/1 W (Each BW) 1 A/1 W (Each BW) 1 A/1 W (Each BW)
All Firing Current 3.5 A - 50 ms (Each BW) 3.5 A - 50 ms (Each BW) 3.5 A - 50 ms (Each BW)
Function Time < 10 ms < 10 ms < 10 ms
Output (16,4 cc chamber) 2.0 MPa 1.0 MPa 1.0 MPa
Electrical Interface MS3111P8-4P Connector per MIL-DTL-26482 Pin Type Shielded Twisted Pair
Cable
Operational Temperature -60 / +70ºC -60 / +70ºC -60 / +70ºC
Environmental Tests MIL-DTL-23659 MIL-DTL-23659 MIL-DTL-23659
Technical Specifications
99
Detonation Systems
Detonation Systems, Exploding Foil Initiators (EFI) and Low Energy Exploding Foil Initiators (LEEFI), are used to activate warhead or rocket motors. The systems are resistant to electromagnetic interference and are activated with high voltage.
System Properties
• Function time < 5µsec
• Hermetically Sealed
• Complies with MIL-DTL-23659, MIL-STD-1316 and MIL-STD-1901A
PYROTECHNIC SYSTEMS
100
Technical Specifications
RS-PC100 Explosive Bolt
RS-PC110 Explosive Bolt
RS-PC160 Explosive Bolt
RS-PIC100 Ejection Device
RS-PV100 Pyro Valve
PropertiesType: Non-
Fragmenting Tensile Load ≥ 2,000 N
Type: Non-Fragmenting
Tensile Load ≥ 10,000 N
Type: Non-Fragmenting Tensile
Load ≥ 91,000 N Double Bridgewire
Tensile Load ≥ 20,000 NMin. Force: 10,000 N
Double BridgewireDouble Bridgewire
Weight < 100 g < 100 g < 300 g < 300 g < 350 g
Function Time < 10 ms < 10 ms < 10 ms < 10 ms < 10 ms
Bridgewire @21°C 1.1 ± 0.1 Ω 1.1 ± 0.1 Ω 1.1 ± 0.1 Ω per each 1.1 ± 0.1 Ω per each 1.1 ± 0.1 Ω per each
Maximum No-Fire @21°C
1A/1W 5 Minutes 1A/1W 5 Minutes 1A/1W 5 Minutes 1A/1W 5 Minutes 1A/1W 5 Minutes
All Fire Current 3.5 A (50 ms) 3.5 A (50 ms) 3.5 A (50 ms) per Each Bridgewire
3.5 A (50 ms) per Each Bridgewire
3.5 A (50 ms) per Each Bridgewire
Operational Temperature Range -54 °C / +71 °C -54 °C / +71 °C -54 °C / +71 °C -54 °C / +71 °C -54 °C / +71 °C
Shelf Life 15 Years 15 Years 15 Years 15 Years 15 Years
Pyrotechnic Compositions
• Magnesium/Teflon/Viton (MTV)
• Boron/Potassium Nitrate (BKNO3)
• Zirconium/Potassium Perchlorate (ZPP)
• MIL-P-46994B Compliant Formulation, II-B, II-D and II-T Size Pellets
• Doughnut Shaped Pellets
• Nanothermite Compositions
• Special Primer Compositions
101
RS-PI100Pin Pusher
RS-PI172Pin Pusher
RS-PI300 Pin Pusher
RS-KK100 Cable Cutter
RS-PCK100 Pin Puller
RS-AS100 Separation
Nut
PropertiesStroke: 3mm
Min. Force: 500N
Cuts 0.05" (1.27 mm) diameter 6061-T6
Aluminum Pin
Stroke: 3mm Min. Force:
3,500N
3 mm diameter AISI 302/304 SS Steel Wire Cutter
Stroke: 13 mm (backwards)
Lateral Load on Pin ≤ 1,000 N
Tip: Non-Fragmenting
Tensile Load ≥ 75,000 N
Weight < 20 g < 0.4 g < 50 g < 100 g < 100 g < 600 g
Function Time < 5 ms < 1 ms < 15 ms < 10 ms < 10 ms < 10 ms
Bridgewire @21°C 1.1 ± 0.1 Ω 4 ± 9.5 Ω 1.1 ± 0.1 Ω 1.1 ± 0.1 Ω 1.1 ± 0.1 Ω 1.1 ± 0.1 Ω
Maximum No Fire @21°C
1A/1W5 Minutes
0.010 Ampere 10 s
1A/1W 5 Minutes
1A/1W5 Minutes
1A/1W5 Minutes
1A/1W5 Minutes
All Fire Current 3.5 A (50 ms)3.0 V DC
(100 μF capacitor) 150 mA (10 ms)
3.5 A (50 ms) 3.5 A (50 ms) 3.5 A (50 ms) 3.5 A (50 ms)
Operational Temperature Range -54 °C / +71 °C -54 °C / +71 °C -54 °C / +71 °C -54 °C / +71 °C -54 °C / +71 °C -54 °C / +71 °C
Shelf Life 15 Years 10 Years 15 Years 15 Years 15 Years 15 Years
PYROTECHNIC SYSTEMS
102
FUZE SYSTEMS
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.
103
FUZE SYSTEMS
Action Impact, Impact, Impact Precision/Delayed Precision/DelayedArming Spin Acceleration Acceleration and SpinArm 14,000 rpm 25 g 120,000 g, 830 rpsOperational Temperature -40 to +60 °C -40 to +60 °C -40 to +60 °CWeight 637 gr 740 gr 22 grFuze Length 123 mm 196 mm 31.6 mmIntrusion Length 46 mm 55 mm 9.6 mmDiameter Ø40 mm Ø64 mm Ø17 mm
107 mm Rocket Fuze
122 mm Rocket Fuze
20 mm M56 Ammo Fuze (M505 A3)
Technical Specifications
Action Impact, Time (0-200 s), Impact, Time (0-200 s), Proximity (1-15 m) Proximity (1-15 m)Arming Acceleration Acceleration Arm 25g 25 gOperational Temperature -40 to +60 °C -40 to +60 °CWeight 740 gr 2,400 grFuze Length 233 mm 224 mmIntrusion Length 54 mm 57 mmDiameter Ø64 mm Ø80 mm
122 mm Proximity Rocket/Missile Fuze
300 mm Proximity Rocket/Missile Fuze
FUZE SYSTEMS
Programmable, delayed and precision mechanical fuzes for 107 mm and 122 mm rockets; electromechanical proximity fuzes/missiles (122 mm and 300 mm); fuzes for Anti-Submarine Warfare (ASW) Rockets; tactical
missiles; anti-tank missiles and unmanned aerial vehicles’ munitions are produced in accordance with MIL-STD-331 and MIL-STD-1316.
Technical Specifications
104
PRODUCTCATALOG
ROKE
TSAN
PRO
DUCT
CAT
ALOG
ENG
2019 ENG-v2
Kemalpaşa Mahallesi Şehit Yüzbaşı Adem Kutlu Sokak No:21 06780 Elmadağ, ANKARA / TURKEYPhone : + 90 (312) 860 55 00Fax : + 90 (312) 863 42 08e-mail : [email protected] : www.roketsan.com.tr
ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.